View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 32953U 08025A 23091.10292506 .00000024 00000-0 10000-3 0 9997
2 32953 82.5100 5.0419 0019906 355.8049 4.2863 12.43121305674077
| Epoch (UTC): | 01 April 2023 02:28:12 |
| Eccentricity: | 0.0019906 |
| inclination: | 82.5100° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 5.0419° |
| argument of perigee: | 355.8049° |
| revolutions per day: | 12.43121305 |
| mean anomaly at epoch: | 4.2863° |
| orbit number at epoch: | 67407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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